View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 23097U 94026A 21122.40505123 0.00000000 00000-0 00000-0 0 03
2 23097 63.5798 345.3266 6980622 260.5731 20.7339 2.00618268 04
Epoch (UTC): | 02 May 2021 09:43:16 |
Eccentricity: | 0.6980622 |
inclination: | 63.5798° |
perigee height: | 1640 km |
apogee height: | 38714 km |
right ascension of ascending node: | 345.3266° |
argument of perigee: | 260.5731° |
revolutions per day: | 2.00618268 |
mean anomaly at epoch: | 20.7339° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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